Spacecraft Structures and Mechanisms From Concept to Launch

Spacecraft Structures and Mechanisms From Concept to Launch by Thomas P. Sarafin, published by Springer Netherlands in May 1995, is a comprehensive resource spanning 850 pages. This book describes the integral process of developing cost-effective and reliable structures and mechanical products for space programs, detailing processes, methods, and providing examples from the field.
Readers will find a thorough exploration of topics essential for ensuring successful missions while managing costs through intelligent design. The content covers various aspects, including requirements documentation, load analysis, and verification planning, making it suitable for system engineers, mechanical designers, and program managers. The book emphasizes the importance of structural reliability and quality assurance in the context of spacecraft development, offering insights into risk management and launch readiness.
Official synopsis Publisher
Spacecraft Structures and Mechanisms describes the integral process of developing cost-effective, reliable structures and mechanical products for space programs. Processes are defined, methods are described and examples are given. It has been written by 24 engineers in the space industry, who cover the themes of (1) ensuring a successful mission, and (2) reducing total cost through good designs and intelligent risk management. Topics include: Introduction and requirements (development process, requirements documentation, requirements definition, space mission environments); Analysis (statics, dynamics and load analysis, fatigue and fracture mechanics, mechanics of materials, strength analysis, heat transfer and thermal effects); Verification and quality assurance (verification planning, structural, mechanical and environmental testing, quality assurance and configuration control, compliance documentation, structural reliability analysis, verification criteria – factors of safety, margins of safety, fracture control, test options); Design (spacecraft configuration development, finite element analysis, mechanism development, designing for producibility, structural design, materials, designing to control loads, load cycles, sensitivity analysis); Final verification (model correlation, risk management, launch readiness reviews).
For system engineers, mechanical designers, stress analysts, dynamics and load analysts, technical leads, program managers.
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